| Section 2. Operating Limitations | ||||||
| Engine | ||||||
| Thrust Setting | Time Limit (Minutes) | Maximum Observed ITT °C | N2% | N1% | Oil Pressure (2) PSI | Oil Temperature (°C) |
| Takeoff | (1) | to | to | |||
| Maximum Continuous | to | to | ||||
| Idle | (Min) | (Min) | to | |||
| Starting (4) | - SEC - SEC - SEC |
(3) | (Min) | |||
| Transient | ( SEC Max) | for SEC | (Max) ( MIN Max) | |||
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Notes: (1) Time limit starts when throttles first advanced for takeoff thrust. (2) Normal Flight: Normal oil pressure is to PSI at N2 speeds above %. Oil pressure below PSI is undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil pressure below PSI is unsafe. (3) Under cold starting conditions, oil pressure between PSI and PSI is limited to seconds. (4) The ITT during ground starts should normally not exceed °C. |
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Normal hydraulic pressure to PSI Normal nitrogen pressure to PSI Normal oxygen pressure to PSI Min battery voltage for battery start volts Max gen load prior to starting second engine amps Motoring of the starter is limited to: First, seconds then minutes cooling. Second, seconds then minutes cooling. Third, seconds then minutes cooling. Emergency Fuel / Minimum Fuel lbs / lbs Maximum Fuel Imbalance - T.O./Touch & Go lbs Max Fuel Imbalance - Flight lbs Max Fuel Imbalance - Landing lbs Fuel crossfeed with 2 engines operating is limited to level flight with less than lbs of fuel remains in the wing tank supplying fuel. Max Ramp Weight lbs Max Takeoff Weight lbs Max Landing Weight lbs |
Extend flaps to 10 degrees KIAS Extend flaps > 10 degrees KIAS Flaps extended > 10 degrees KIAS Aircraft is limited to KIAS or MACH, whichever is less. Landing Gear/Lights KIAS / FL Wipers KIAS Tire Knots GS Max Tailwind Knots Max Crosswind (Dry) Knots Max Crosswind (Wet) Knots Max Crosswind (Icy) Knots Max Operating Altitude FL Yaw Damper required operable for flight above FL Do not use autopilot below FT AGL Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above °C OAT/SAT. Do not operate surface anti-ice systems in flight at ram air temperatures above °C. To ensure proper wing anti-ice operation, the throttles must be kept at % N2 minimum. |
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